CA2177211A1 - Missile Test Method and Apparatus - Google Patents
Missile Test Method and ApparatusInfo
- Publication number
- CA2177211A1 CA2177211A1 CA2177211A CA2177211A CA2177211A1 CA 2177211 A1 CA2177211 A1 CA 2177211A1 CA 2177211 A CA2177211 A CA 2177211A CA 2177211 A CA2177211 A CA 2177211A CA 2177211 A1 CA2177211 A1 CA 2177211A1
- Authority
- CA
- Canada
- Prior art keywords
- missile
- performance
- access cover
- tests
- repeated
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41G—WEAPON SIGHTS; AIMING
- F41G7/00—Direction control systems for self-propelled missiles
- F41G7/001—Devices or systems for testing or checking
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- General Engineering & Computer Science (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Abstract
A missile (50) is tested by first stimulating the performance of missile (50) built-in tests that are stimulated in service by signals from the launch site, and which tests do not require internal access to the missile (50). If performance is satisfactory, no further testing is required. If a condition of unsatisfactory missile (50) performance is detected, an access cover (63) is removed, connections are made to internal sources of data, and the built-in tests are repeated in order to determine which internal components caused the unsatisfactory missile (50) performance. The component is repaired. The testing with the access cover (63) removed is repeated, and, if the performance is satisfactory, the access cover (63) is replaced and the testing with the access cover (63) present is repeated.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US08/478,148 US5721680A (en) | 1995-06-07 | 1995-06-07 | Missile test method for testing the operability of a missile from a launch site |
US08/478,148 | 1995-06-07 |
Publications (2)
Publication Number | Publication Date |
---|---|
CA2177211A1 true CA2177211A1 (en) | 1996-12-08 |
CA2177211C CA2177211C (en) | 1999-03-23 |
Family
ID=23898737
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CA002177211A Expired - Fee Related CA2177211C (en) | 1995-06-07 | 1996-05-23 | Missile test method and apparatus |
Country Status (6)
Country | Link |
---|---|
US (1) | US5721680A (en) |
EP (1) | EP0747656A3 (en) |
JP (1) | JP2875508B2 (en) |
AU (1) | AU673794B1 (en) |
CA (1) | CA2177211C (en) |
IL (1) | IL118498A (en) |
Families Citing this family (37)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5992290A (en) * | 1997-04-09 | 1999-11-30 | Cubic Defense Systems, Inc. | Aircraft interface device and crossover cable kit |
US6006145A (en) * | 1997-06-30 | 1999-12-21 | The United States Of America As Represented By The Secretary Of The Navy | Method and apparatus for directing a pursuing vehicle to a target with intelligent evasion capabilities |
SE513330C2 (en) * | 1998-05-15 | 2000-08-28 | Saab Ab | Method of simulating a real robot by means of a robot simulator when testing an aircraft system comprising a weapon system |
DE19857894A1 (en) * | 1998-12-15 | 2000-06-21 | Bodenseewerk Geraetetech | Aircraft launched missile system that has built in controller for reconfiguration and allows function monitoring and error detection |
US6519554B1 (en) * | 1999-05-17 | 2003-02-11 | The United States Of America As Represented By The Secretary Of The Navy | Computer implemented system and method for evaluating gas generator launchers |
US20040034824A1 (en) * | 2002-08-14 | 2004-02-19 | The Boeing Company | System, method and computer program product for receiving and displaying store delivery system built-in-test data |
US6896220B2 (en) * | 2003-05-23 | 2005-05-24 | Raytheon Company | Munition with integrity gated go/no-go decision |
US6796213B1 (en) * | 2003-05-23 | 2004-09-28 | Raytheon Company | Method for providing integrity bounding of weapons |
US6941850B1 (en) * | 2004-01-09 | 2005-09-13 | Raytheon Company | Self-contained airborne smart weapon umbilical control cable |
DE102004042990B4 (en) * | 2004-09-06 | 2008-11-20 | Michael Grabmeier | Method and device for testing an operational cruise missile in various test scenarios by means of maintenance mode |
US7183970B1 (en) * | 2005-01-31 | 2007-02-27 | The United States Of America As Represented By The Secretary Of The Navy | Missile time-space-position-information unit test software |
US20070243505A1 (en) * | 2006-04-13 | 2007-10-18 | Honeywell International Inc. | System and method for the testing of air vehicles |
US7813888B2 (en) * | 2006-07-24 | 2010-10-12 | The Boeing Company | Autonomous vehicle rapid development testbed systems and methods |
US7643893B2 (en) * | 2006-07-24 | 2010-01-05 | The Boeing Company | Closed-loop feedback control using motion capture systems |
DE102006041140B4 (en) * | 2006-09-01 | 2009-11-26 | Lfk-Lenkflugkörpersysteme Gmbh | Procedure for checking the functioning of unmanned armed missiles |
US7885732B2 (en) * | 2006-10-25 | 2011-02-08 | The Boeing Company | Systems and methods for haptics-enabled teleoperation of vehicles and other devices |
DE102006054340A1 (en) * | 2006-11-17 | 2008-05-21 | Lfk-Lenkflugkörpersysteme Gmbh | A method for verifying the ability to interact between an aircraft and an armed unmanned missile coupled thereto |
DE102007022672C5 (en) * | 2007-05-15 | 2010-09-09 | Lfk-Lenkflugkörpersysteme Gmbh | Procedure for condition monitoring of an intelligent weapon and intelligent weapon |
KR100873430B1 (en) | 2007-05-23 | 2008-12-11 | 한국과학기술원 | Flexible Launch Vehicle Ground Test-bed and Adaptive Controller |
US20090319096A1 (en) * | 2008-04-25 | 2009-12-24 | The Boeing Company | Control and monitor heterogeneous autonomous transport devices |
US8068983B2 (en) * | 2008-06-11 | 2011-11-29 | The Boeing Company | Virtual environment systems and methods |
US8731745B2 (en) * | 2008-07-01 | 2014-05-20 | Aerojet Rocketdyne Of De, Inc. | Sequence diagram system |
US7881887B2 (en) * | 2008-07-14 | 2011-02-01 | Sikorsky Aircraft Corporation | Wireless wireharness testing system |
DE102008054264B4 (en) * | 2008-10-31 | 2012-09-13 | Lfk-Lenkflugkörpersysteme Gmbh | Multifunctional service and test facility for unmanned aerial vehicles |
US8563909B2 (en) * | 2010-04-09 | 2013-10-22 | Bae Systems Information And Electronic Systems Integration Inc. | Automatic re-initialization of resonant sensors in rocket and missile guidance systems |
CN103357137A (en) * | 2013-07-25 | 2013-10-23 | 成都陵川特种工业有限责任公司 | Apparatus for detecting fire extinguishing launcher |
CN105403111B (en) * | 2015-12-18 | 2016-10-19 | 中国人民解放军63908部队 | Non-maintaining guided missile static properties detection device |
US10156426B2 (en) | 2016-06-21 | 2018-12-18 | The United States Of America, As Represented By The Secretary Of The Navy | Apparatus and methods for parallel testing of devices |
CN106546134A (en) * | 2016-12-05 | 2017-03-29 | 航天恒星科技有限公司 | A kind of missile monitor system simulation and verification platform and verification method |
RU2661414C2 (en) * | 2016-12-19 | 2018-07-16 | Российская Федерация, От Имени Которой Выступает Министерство Промышленности И Торговли Российской Федерации | Rocket simulator |
RU2668010C2 (en) * | 2017-05-12 | 2018-09-25 | Константин Федорович Заренок | Method for determining the possibility of further operation of the anti-aircraft missiles on the basis of automated record of information on the state of its on-board equipment |
KR101937729B1 (en) | 2017-11-02 | 2019-01-11 | 주식회사 한화 | Firing test device and method for missile cable |
CN110749253B (en) * | 2019-10-24 | 2021-11-30 | 中国人民解放军32181部队 | Missile performance test unit for missile test system |
KR102361169B1 (en) * | 2020-10-27 | 2022-02-14 | 엘아이지넥스원 주식회사 | Guided missile storage device |
TWI806012B (en) * | 2021-03-10 | 2023-06-21 | 國家中山科學研究院 | Detonation signal processing test system and method |
CN114739241A (en) * | 2022-03-16 | 2022-07-12 | 上海机电工程研究所 | Missile wireless test system and test method for test island |
CN116608741B (en) * | 2023-07-20 | 2023-10-03 | 东方空间技术(山东)有限公司 | Initiating explosive device time sequence testing system, method and equipment of rocket |
Family Cites Families (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4031806A (en) * | 1976-09-01 | 1977-06-28 | The United States Of America As Represented By The Secretary Of The Army | Internal umbilical connector for missiles |
IL74952A0 (en) * | 1984-05-04 | 1985-08-30 | Gould Inc | Method and system for improving the operational reliability of electronic systems formed of subsystems which perform different functions |
US4745840A (en) * | 1987-02-24 | 1988-05-24 | Varo, Inc. | Modified missile launcher |
US4935881A (en) * | 1987-04-14 | 1990-06-19 | Jeffrey Lowenson | Method and apparatus for testing missile systems |
CA2049270A1 (en) * | 1990-11-01 | 1992-05-02 | Robert W. Petty | Integrated fiber optic missile test system |
US5224860A (en) * | 1991-03-01 | 1993-07-06 | Electronics & Space Corp. | Hardware-in-the-loop tow missile system simulator |
US5490093A (en) * | 1991-04-22 | 1996-02-06 | Hughes Aircraft Company | Method for enhancing computer controlled missile performance |
US5294078A (en) * | 1992-07-07 | 1994-03-15 | Gurr John W | Integrated system and method for assembling, and then transporting and supporting a launch vehicle |
CA2100156C (en) * | 1992-07-13 | 1998-07-28 | Ronald W. Monk | Method and apparatus for missile interface testing |
US5591031A (en) * | 1994-05-31 | 1997-01-07 | Hughes Electronics | Missile simulator apparatus |
US5520115A (en) * | 1995-01-25 | 1996-05-28 | The United States Of America As Represented By The Secretary Of The Army | Timing and safety module to sequence events in missiles |
-
1995
- 1995-06-07 US US08/478,148 patent/US5721680A/en not_active Expired - Lifetime
-
1996
- 1996-05-23 CA CA002177211A patent/CA2177211C/en not_active Expired - Fee Related
- 1996-05-23 AU AU52456/96A patent/AU673794B1/en not_active Ceased
- 1996-05-30 IL IL11849896A patent/IL118498A/en not_active IP Right Cessation
- 1996-06-03 EP EP96303994A patent/EP0747656A3/en not_active Withdrawn
- 1996-06-06 JP JP8143999A patent/JP2875508B2/en not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
US5721680A (en) | 1998-02-24 |
IL118498A (en) | 1999-06-20 |
JP2875508B2 (en) | 1999-03-31 |
JPH0933198A (en) | 1997-02-07 |
AU673794B1 (en) | 1996-11-21 |
CA2177211C (en) | 1999-03-23 |
IL118498A0 (en) | 1996-09-12 |
EP0747656A2 (en) | 1996-12-11 |
EP0747656A3 (en) | 1998-11-25 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
EEER | Examination request | ||
MKLA | Lapsed |
Effective date: 20140523 |